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IRIDIUM 172, 43927

Orbit data source: Space-Track

IRIDIUM 172, 43927 is a payload satellite owned by Iridium (US) in LEO that was launched on Fri, 11 Jan 2019 UTC via an FALCON 9 launch vehicle from the Air Force Western Test Range (AFWTR). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.

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Identifier
43927, 2019-002F
Orbit
LEO
Country
Flag of USUS
Related business
Manufacturer
NGIS SSG Gilbert
Mission
Operational Commercial Communications
Bus & Motor
ELITEBUS, Unknown motor
Mass
860 kg wet, 700 kg dry
Launch date (UTC)
2019-01-11 (7 years ago)
Launch vehicle
FALCON 9
Launch site
Air Force Western Test Range (AFWTR)
Object type
Payload
Rocket body
Debris
Shape & HBR
Trap Box + 2 Pan, 4.8 m
Radar Cross Section
10.154 m², Large (>1 m²)

Expand to show TLE details & history
Last TLE update: 13 hours ago

TLE from 13 hours ago
0 IRIDIUM 172
1 43927U 19002F   25363.71262671  .00000040  00000-0  71082-5 0  9995
2 43927  86.3954  64.4206 0002005  95.7830 264.3595 14.34217517364678
Epoch: 2025-12-29T17:06Z
TLE epoch observation values (Epoch: 2025-12-29T17:06:10.947Z)
Latitude
0.00002°
Longitude
69.46867°
Altitude
780.86 km
Speed
7.463 km/s
True Right ascension
04h 17m 40s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
05:25:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
776.067 km
Perigee altitude
773.198 km
Semi-major axis
7,152.769 km
Eccentricity
0.0002
Inclination
86.3954°
RAAN
64.4206°
Arg. of periapsis
95.783°
True anomaly
264.33664°
Mean anomaly
264.3595°
Eccentric anomaly
264.34807°
Mean motion
3.58783 °/min
Orbital period
100.34 mins
BSTAR
0.0000071082
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